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To realize innovative transportation systems for intercontinental flight and orbital spaceflight, it is essential to establish the necessary aerodynamic, structural, propulsion, and control technologies for a vehicle to fly at high altitudes and speeds within the atmosphere, and to verify them by using small-scale unmanned supersonic experimental aircraft. This paper describes the control technologies for a 3-kg low-speed model airplane flying autonomously from takeoff, through a circuit, to landing. Guidance and control systems are established for the plane, and flight experiments verify that the control laws work well for all flight modes.

transactions of the japan society for aeronautical and space sciences, aerospace technology japan

Design and Tests of Guidance and Control Systems for Autonomous Flight of a Low-Speed Model Airplane for Application to a Small-Scale Unmanned Supersonic Airplane